{"title":"On the Control of a Simplified Rocking Delta Wing Model","authors":"C. Chien, C. Cheng, M.D. Chen, M. Lai","doi":"10.1109/AEROCS.1993.720974","DOIUrl":null,"url":null,"abstract":"In this paper, we propose a nonlinear state feedback control law for an approximated delta wing wingrock control experiment model. The stability of the closed loop system is proved and the performance is demonstrated.","PeriodicalId":170527,"journal":{"name":"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,","volume":"519 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1993-05-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AEROCS.1993.720974","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
In this paper, we propose a nonlinear state feedback control law for an approximated delta wing wingrock control experiment model. The stability of the closed loop system is proved and the performance is demonstrated.
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